Rotary Vane Actuator Cooling Flow for Precise Position Holding
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Existing rotary actuators in hot environments face challenges with cooling fluid flow, as larger pumps are needed to manage heat, leading to sluggish and imprecise position control due to the continuous cooling flow requirement.
Innovation Solution
The implementation of a controllable cooling fluid flow path that connects high and low pressure chambers within a predetermined rotational range of the rotor, allowing cooling flow only when necessary, thereby reducing the size of fluid pumps and minimizing dead band effects.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Temperature
If continuous cooling fluid flow is provided to remove heat from the actuator, then heat removal efficiency is improved, but position control precision deteriorates due to sluggish and imprecise control
Solution Approach 1:
The cooling fluid flow is provided periodically rather than continuously. The system activates cooling flow during periods when the actuator requires heat removal (such as during or after actuation cycles) and shuts off the cooling flow during periods when precise position control is required. This periodic operation allows the actuator to be cooled effectively when needed while maintaining precise positional control when the cooling flow is not active.
2Temperature
If larger fluid pumps are implemented to provide sufficient cooling flow, then heat removal capability is improved, but device weight and cost increase
Solution Approach 1:
Instead of providing excessive cooling flow continuously through larger pumps, the system provides partial cooling action only when and where needed. The cooling flow is activated during specific operational phases when heat generation occurs and deactivated during phases when cooling is not required, allowing the use of smaller, lighter pumps that can deliver adequate cooling during active periods without the need for oversized continuous cooling capacity.
3Temperature
If cooling flow is provided during position control operations, then heat removal is improved, but control precision deteriorates due to dead band effects
Solution Approach 1:
The system implements periodic control of the cooling flow by activating it during actuation cycles when heat is generated and deactivating it during positional holding phases. This timing coordination ensures that cooling flow and precise position control operations do not occur simultaneously, thereby eliminating dead band effects that would otherwise degrade positional holding capability while still maintaining effective heat removal during active operation.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
This solution enables efficient heat removal when needed while maintaining precise position control by activating cooling flow only during specific rotational positions, reducing the need for larger pumps and improving positional holding capability.
Implementation Method 1
the flow of fuel can remove heat, lowering the actuator temperature
Implementation Method 2
cooling orifices that allow a limited flow of fuel through the actuator and the flow of fuel can remove heat
Data Source
Figure 1~12
Figure 2~3
Figure 4A~4B
AI summary
The subject matter of this specification can be embodied in, among other things, a rotary vane actuator (1100) that includes a stator having at least one stator vane (470) and a rotor (410) having at least one rotor vane (420) projecting from a central shaft. The rotor vane (420) is adapted to contact the stator vane (470), and a high pressure chamber (460a/460b) is defined by the stator and a first side of the rotor vane and a low pressure chamber (460b/460a) on a second side of the rotor vane (420). The actuator further includes at least a first aperture (462a/462b) connected to the high pressure chamber (460a/460b) a second aperture (462b/462a) connected to the low pressure chamber (460b/460a). A fluid flow passage connects the first aperture (462a/462b) in the high pressure chamber (460a/460b) to the second aperture (462b/462a) in the low pressure chamber (460b/460a).